Comparison of three thrust calculation methods using in-flight thrust data
Donald Lee Hughes, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Hugh L. Dryden Flight Research Center
National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981 - Technology & Engineering - 32 pages
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absolute value adjustment procedures afterburners aircraft gross thrust airplane altitude calculated gross thrust calculating engine gross compressor face constant cruise flight conditions Dryden Flight Research ducted fans engine gross thrust engine number equal measured gross equation extrapolated to cruise F GGM Flight Research Center four engines gas constant Gas Generator Method gravitational constant gross thrust calculated gross thrust coefficient gross thrust equal gross thrust method gross thrust value ground thrust calibration ground thrust data IN-FLIGHT THRUST DATA KC-135A aircraft kN/m Mach number Mass Momentum Method measured gross thrust METHODS USING IN-FLIGHT NASA nozzle coefficient nozzle discharge nozzle exit percent of full pressure-area method range of thrust ratio of specific SGTM simplified gross thrust specific heat station F three methods THREE THRUST CALCULATION THRUST CALCULATION METHODS thrust stand calibrations total aircraft gross total gross thrust turbine turbofan turbojet values of gross values of thrust winglets installed